AirfRANS: High Fidelity Computational Fluid Dynamics Dataset for Approximating Reynolds-Averaged Navier-Stokes Solutions

Florent Bonnet, Ahmed Jocelyn Mazari, Paola Cinnella, Patrick Gallinari
12/15/2022
cs.LGcs.CVphysics.comp-ph

Official code: Extrality/AirfRANS (73 stars, ODbL-1.0, last commit 2025-01-09). 2 more implementations below.

Abstract

Surrogate models are necessary to optimize meaningful quantities in physical dynamics as their recursive numerical resolutions are often prohibitively expensive. It is mainly the case for fluid dynamics and the resolution of Navier-Stokes equations. However, despite the fast-growing field of data-driven models for physical systems, reference datasets representing real-world phenomena are lacking. In this work, we develop AirfRANS, a dataset for studying the two-dimensional incompressible steady-state Reynolds-Averaged Navier-Stokes equations over airfoils at a subsonic regime and for different angles of attacks. We also introduce metrics on the stress forces at the surface of geometries and visualization of boundary layers to assess the capabilities of models to accurately predict the meaningful information of the problem. Finally, we propose deep learning baselines on four machine learning tasks to study AirfRANS under different constraints for generalization considerations: big and scarce data regime, Reynolds number, and angle of attack extrapolation.

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Code Implementations(3)

Extrality/AirfRANSOfficial100%
ODbL-1.0

In this repository, you will find the different python scripts to train the available models on the AirfRANS dataset proposed at the NeurIPS 2022 Datasets and Benchmarks Track conference.

7312Python, Jupyter NotebookAug 4, 20221 years agoODbL-1.0
ODbL-1.0

Python scripts to run resolution of the Reynolds-Averaged-Navier-Stokes equations over NACA 4 and 5 digits airfoils.

279C++, PythonAug 5, 20221 years agoODbL-1.0
MIT

The AirfRANS dataset makes available numerical resolutions of the incompressible Reynolds-Averaged Navier–Stokes (RANS) equations over the NACA 4 and 5 digits series of airfoils and in a subsonic flight regime setup.

225PythonDec 28, 20221 years agoMIT

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Cite this paper

@article{bonnet2022airfrans,
  title  = {AirfRANS: High Fidelity Computational Fluid Dynamics Dataset for Approximating Reynolds-Averaged Navier-Stokes Solutions},
  author = {Florent Bonnet and Ahmed Jocelyn Mazari and Paola Cinnella and Patrick Gallinari},
  year   = {2022},
  eprint = {2212.07564},
  archivePrefix = {arXiv},
  url    = {https://arxiv.org/abs/2212.07564}
}

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